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From Demonstration of Function into Operation

Involved Parties 1/2

Airspace Regulator (States coordinated through EUROCONTROL in future European Commission within Single European Sky Air Traffic Management SESAM) defines framework for Air Traffic Service Provider and airspace users

ATS offers service

Slide 5

Involved Parties 2/2

Aircraft / Equipment manufactures to design airborne system

Standardised function through certification (EASA, FAA,… - State of Registry)

Operational Procedures implemented through Operational requirements e.g. EU-OPS and implemented through National home Authority of the operator

Pilot Training and Licensing under overview of National home authority

Slide 6

EASA responsibilities as defined today

“Rulemaking” for European Member States + Norway, Iceland, Bulgaria, Romania, Switzerland as defined in Basic Regulation EC 1592/2002 and related implementation regulations EC 1702/2003 and 2042/2003 in the area of aircraft design, production and maintenance

Certification of Aircraft and Design Organisations

Standardisation of National Authorities and coordination of SAFETY ASSESSMENT OF FOREIGN AIRCRAFT (SAFA) program

Aircraft Certification Principles 1/3

CS 25.1301 Function and installation:Each item of installed equipment must –(a) Be of a kind and design appropriate to its intended function;

Slide 9

Aircraft Certification Principles 1/3

CS 25.1309 Equipment, systems and installations(a) The aeroplane equipment and systems must be designed and installed so that:(1) Those required for type certification or by operating rules, or whose improper functioning would reduce safety, perform as intended under the aeroplane operating and environmental conditions.(2) Other equipment and systems are not a source of danger in themselves and do not adversely affect the proper functioning of those covered by sub-paragraph (a)(1) of this paragraph.(b) The aeroplane systems and associated components, considered separately and in relation to other systems, must be designed so that –(1) Any catastrophic failure condition (i) is extremely improbable; and (ii) does not result from a single failure; and(2) Any hazardous failure condition is extremely remote; and(3) Any major failure condition is remote.